electrified aircraft

Fleet Analysis of a Hybrid Turboelectric Commercial Regional Jet under NASA ULI Program
Under the NASA University Leadership Initiative (ULI) program, researchers from multiple institutes are collaborating on development of …
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Performance Assessment of a Distributed Electric Propulsion System for a Medium Altitude Long Endurance Unmanned Aerial Vehicle
Distributed propulsion systems are enabled by electrified aircraft and can provide aero-propulsive benefits. The magnitude and impact …
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An Update on Sizing and Performance Analysis of a Hybrid Turboelectric Regional Jet for the NASA ULI Program
Under the NASA University Leadership Initiative (ULI) program, a team of universities are collaborating on the advancement of …
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Design and Analysis of the Thermal Management System of a Hybrid Turboelectric Regional Jet for the NASA ULI Program
A team of researchers from multiple universities are collaborating on the demonstration of a hybrid turboelectric regional jet for 2030 …
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Feasibility Assessments of a Hybrid Turboelectric Medium Altitude Long Endurance Unmanned Aerial Vehicle
Electrified propulsion systems can provide potential environmental and performance benefits for future aircraft. The choice of the …
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A Framework for Electrified Propulsion Architecture and Operation Analysis
Purpose – The purpose of this paper was to create a generic and flexible framework for the exploration, evaluation and side-by-side …
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A Methodology For Dynamic Sizing of Electric Power Generation and Distribution Architectures
Electric and hybrid electric aircraft pose a significant architecture challenge, as these concepts not only deal with considerably high …
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Sizing and Optimization of Novel General Aviation Vehicles and Propulsion System Architectures
The drive for more efficient flying vehicles in all categories may necessitate a significant departure from the tube-and-wing or …
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Development of Parametric Power Generation and Distribution Subsystem Models at the Conceptual Aircraft Design Stage
The ongoing efforts to reduce aviation related greenhouse gas emissions and fuel burn have led to advancements in power generation and …
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Sizing, integration and performance evaluation of hybrid electric propulsion subsystem architectures
This paper presents a methodology for the sizing and synthesis of power generation and distribution (PG&D) subsystems. The PG&D …
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